RU2009112629A - Камера сгорания газовой турбины - Google Patents
Камера сгорания газовой турбины Download PDFInfo
- Publication number
- RU2009112629A RU2009112629A RU2009112629/06A RU2009112629A RU2009112629A RU 2009112629 A RU2009112629 A RU 2009112629A RU 2009112629/06 A RU2009112629/06 A RU 2009112629/06A RU 2009112629 A RU2009112629 A RU 2009112629A RU 2009112629 A RU2009112629 A RU 2009112629A
- Authority
- RU
- Russia
- Prior art keywords
- zone
- combustion chamber
- post
- flame tube
- compressed air
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006042124.8 | 2006-09-07 | ||
DE102006042124A DE102006042124B4 (de) | 2006-09-07 | 2006-09-07 | Gasturbinenbrennkammer |
Publications (1)
Publication Number | Publication Date |
---|---|
RU2009112629A true RU2009112629A (ru) | 2010-10-20 |
Family
ID=38982562
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2009112629/06A RU2009112629A (ru) | 2006-09-07 | 2007-09-04 | Камера сгорания газовой турбины |
Country Status (8)
Country | Link |
---|---|
US (1) | US20100126174A1 (ja) |
EP (1) | EP2059724A1 (ja) |
JP (1) | JP2010502928A (ja) |
CN (1) | CN101573560A (ja) |
CA (1) | CA2662720A1 (ja) |
DE (1) | DE102006042124B4 (ja) |
RU (1) | RU2009112629A (ja) |
WO (1) | WO2008028621A1 (ja) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7617684B2 (en) | 2007-11-13 | 2009-11-17 | Opra Technologies B.V. | Impingement cooled can combustor |
DE102009035550A1 (de) * | 2009-07-31 | 2011-02-03 | Man Diesel & Turbo Se | Gasturbinenbrennkammer |
EP2405200A1 (en) | 2010-07-05 | 2012-01-11 | Siemens Aktiengesellschaft | A combustion apparatus and gas turbine engine |
NL2005381C2 (en) | 2010-09-21 | 2012-03-28 | Micro Turbine Technology B V | Combustor with a single limited fuel-air mixing burner and recuperated micro gas turbine. |
US9625153B2 (en) * | 2010-11-09 | 2017-04-18 | Opra Technologies B.V. | Low calorific fuel combustor for gas turbine |
US9423132B2 (en) * | 2010-11-09 | 2016-08-23 | Opra Technologies B.V. | Ultra low emissions gas turbine combustor |
US8844260B2 (en) * | 2010-11-09 | 2014-09-30 | Opra Technologies B.V. | Low calorific fuel combustor for gas turbine |
DE102011007562A1 (de) * | 2011-04-18 | 2012-10-18 | Man Diesel & Turbo Se | Brennkammergehäuse und damit ausgerüstete Gasturbine |
US9328663B2 (en) | 2013-05-30 | 2016-05-03 | General Electric Company | Gas turbine engine and method of operating thereof |
US9366184B2 (en) | 2013-06-18 | 2016-06-14 | General Electric Company | Gas turbine engine and method of operating thereof |
DE102014204482A1 (de) | 2014-03-11 | 2015-09-17 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammer einer Gasturbine |
EP2952812B1 (en) * | 2014-06-05 | 2018-08-08 | General Electric Technology GmbH | Annular combustion chamber of a gas turbine and liner segment |
US10337738B2 (en) | 2016-06-22 | 2019-07-02 | General Electric Company | Combustor assembly for a turbine engine |
US11022313B2 (en) | 2016-06-22 | 2021-06-01 | General Electric Company | Combustor assembly for a turbine engine |
CN107101224B (zh) * | 2017-05-23 | 2023-01-10 | 新奥能源动力科技(上海)有限公司 | 一种单管燃烧室和燃气轮机 |
DE102017125051A1 (de) | 2017-10-26 | 2019-05-02 | Man Diesel & Turbo Se | Strömungsmaschine |
DE102018125698A1 (de) | 2018-10-17 | 2020-04-23 | Man Energy Solutions Se | Gasturbinenbrennkammer |
US11181269B2 (en) | 2018-11-15 | 2021-11-23 | General Electric Company | Involute trapped vortex combustor assembly |
CN110657450B (zh) * | 2019-10-31 | 2023-09-15 | 中国华能集团有限公司 | 一种燃气轮机的燃烧室及其工作方法 |
CN110848030B (zh) * | 2019-11-25 | 2021-09-21 | 东方电气集团东方汽轮机有限公司 | 一种燃气轮机燃烧室火焰筒冲击冷却系统优化方法 |
CN113701195A (zh) * | 2021-09-03 | 2021-11-26 | 永旭腾风新能源动力科技(北京)有限公司 | 双燃料管燃烧室及燃气轮机 |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5129726A (ja) * | 1974-09-06 | 1976-03-13 | Mitsubishi Heavy Ind Ltd | |
GB1490145A (en) * | 1974-09-11 | 1977-10-26 | Mtu Muenchen Gmbh | Gas turbine engine |
US4030875A (en) * | 1975-12-22 | 1977-06-21 | General Electric Company | Integrated ceramic-metal combustor |
GB1581531A (en) * | 1976-09-09 | 1980-12-17 | Rolls Royce | Control of airflow in combustion chambers by variable rate diffuser |
US4628687A (en) * | 1984-05-15 | 1986-12-16 | A/S Kongsberg Vapenfabrikk | Gas turbine combustor with pneumatically controlled flow distribution |
EP0182570A2 (en) * | 1984-11-13 | 1986-05-28 | A/S Kongsberg Väpenfabrikk | Gas turbine engine combustor |
DE3663847D1 (en) * | 1985-06-07 | 1989-07-13 | Ruston Gas Turbines Ltd | Combustor for gas turbine engine |
US5138841A (en) * | 1990-01-23 | 1992-08-18 | The Commonwealth Of Australia | Gas turbine engines |
US5687572A (en) * | 1992-11-02 | 1997-11-18 | Alliedsignal Inc. | Thin wall combustor with backside impingement cooling |
US5450724A (en) * | 1993-08-27 | 1995-09-19 | Northern Research & Engineering Corporation | Gas turbine apparatus including fuel and air mixer |
GB2297151B (en) * | 1995-01-13 | 1998-04-22 | Europ Gas Turbines Ltd | Fuel injector arrangement for gas-or liquid-fuelled turbine |
GB9505067D0 (en) * | 1995-03-14 | 1995-05-03 | Europ Gas Turbines Ltd | Combustor and operating method for gas or liquid-fuelled turbine |
US6378286B2 (en) * | 1995-06-16 | 2002-04-30 | Power Tech Associates, Inc. | Low NOX gas turbine combustor liner |
GB2311596B (en) * | 1996-03-29 | 2000-07-12 | Europ Gas Turbines Ltd | Combustor for gas - or liquid - fuelled turbine |
GB2328011A (en) * | 1997-08-05 | 1999-02-10 | Europ Gas Turbines Ltd | Combustor for gas or liquid fuelled turbine |
US6098397A (en) * | 1998-06-08 | 2000-08-08 | Caterpillar Inc. | Combustor for a low-emissions gas turbine engine |
US6314716B1 (en) * | 1998-12-18 | 2001-11-13 | Solar Turbines Incorporated | Serial cooling of a combustor for a gas turbine engine |
GB2356924A (en) * | 1999-12-01 | 2001-06-06 | Abb Alstom Power Uk Ltd | Cooling wall structure for combustor |
US6826913B2 (en) * | 2002-10-31 | 2004-12-07 | Honeywell International Inc. | Airflow modulation technique for low emissions combustors |
GB0319329D0 (en) * | 2003-08-16 | 2003-09-17 | Rolls Royce Plc | Variable geometry combustor |
US7036316B2 (en) * | 2003-10-17 | 2006-05-02 | General Electric Company | Methods and apparatus for cooling turbine engine combustor exit temperatures |
US20070151251A1 (en) * | 2006-01-03 | 2007-07-05 | Haynes Joel M | Counterflow injection mechanism having coaxial fuel-air passages |
US7617684B2 (en) * | 2007-11-13 | 2009-11-17 | Opra Technologies B.V. | Impingement cooled can combustor |
US20110067405A1 (en) * | 2009-09-18 | 2011-03-24 | Concepts Eti, Inc. | Integrated Ion Transport Membrane and Combustion Turbine System |
-
2006
- 2006-09-07 DE DE102006042124A patent/DE102006042124B4/de active Active
-
2007
- 2007-09-04 WO PCT/EP2007/007696 patent/WO2008028621A1/de active Application Filing
- 2007-09-04 CA CA002662720A patent/CA2662720A1/en not_active Abandoned
- 2007-09-04 RU RU2009112629/06A patent/RU2009112629A/ru not_active Application Discontinuation
- 2007-09-04 CN CNA2007800417484A patent/CN101573560A/zh active Pending
- 2007-09-04 JP JP2009527046A patent/JP2010502928A/ja active Pending
- 2007-09-04 EP EP07818048A patent/EP2059724A1/de not_active Ceased
- 2007-09-04 US US12/440,314 patent/US20100126174A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
CN101573560A (zh) | 2009-11-04 |
WO2008028621A1 (de) | 2008-03-13 |
DE102006042124A1 (de) | 2008-03-27 |
JP2010502928A (ja) | 2010-01-28 |
EP2059724A1 (de) | 2009-05-20 |
US20100126174A1 (en) | 2010-05-27 |
CA2662720A1 (en) | 2008-03-13 |
DE102006042124B4 (de) | 2010-04-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FA93 | Acknowledgement of application withdrawn (no request for examination) |
Effective date: 20100907 |